Mario Tindaro Migliorino | Ricerc@Sapienza

Pubblicazioni

Titolo	Pubblicato in	Anno
Experimental Methodological Investigations of Sloshing-Induced Mass Transfer Coefficients for Aircraft Tanks	JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER	2025
Integrated Optimization of a Three-Stage Clustered Hybrid Rocket Launcher using Neural Networks	AIAA SciTech Forum 2024	2024
Computational Analysis and Regression Laws for Nozzle Erosion Prediction in Hybrid Rockets	JOURNAL OF PROPULSION AND POWER	2024
Modeling and Analysis of Film Cooling in Oxygen-Kerosene Rocket Thrust Chambers	AIAA SciTech Forum 2024	2024
Radiative Wall Heat Transfer Evaluation in Hybrid Rocket Thrust Chambers	AIAA SciTech Forum 2024	2024
Experimental investigations on the sloshing-induced pressure drop in tanks for hydrogen-powered aircraft	AIAA SciTech Forum 2024	2024
Multi-disciplinary optimization of single-stage hybrid rockets for lunar ascent	ACTA ASTRONAUTICA	2024
Computational Analysis of High-Altitude Test Facilities	Space Propulsion Conference 2024	2024
Experimental Investigation of a H2O2 Hybrid Rocket with Different Swirl Injections and Fuels	APPLIED SCIENCES	2024
NUMERICAL ACTIVITIES ON THE PARAFFIN-BASED FUEL MTM IN THE FRAMEWORK OF THE PHAEDRA PROJECT	Proceedings of the 2024 Space Propulsion Conference	2024
Conjugate heat transfer numerical simulations of a methane-oxygen liquid rocket engine	Proceedings of the 2024 Space Propulsion Conference	2024
Numerical Modeling of Scale Effects in Paraffin-Hydrogen Peroxide Hybrid Rockets with Swirl Injection	Proceedings of the International Astronautical Conference	2024
Multi-disciplinary Optimization of Single-stage Hybrid Rocket with Swirl Injection for Lunar Ascent	AIAA Scitech 2023 Forum	2023
Numerical Simulations of a Paraffin-Hydrogen Peroxide Hybrid Rocket with Swirl Injection	Proceedings of the AIAA Scitech 2023 Forum	2023
Numerical Analysis of Film Cooling and Mixture Ratio Bias in Oxygen-Methane Liquid Rocket Engines	AIAA Scitech 2023 Forum	2023
Numerical and experimental analysis of fuel regression rate in a lab-scale hybrid rocket engine with swirl injection	AEROSPACE SCIENCE AND TECHNOLOGY	2023
Modeling of swirl injection effects in a H2O2-HDPE hybrid rocket	Proceedings of the Aerospace Europe Conference 2023 - 10th EUCASS - 9th CEAS	2023
Numerical Simulations of Fuel Shape Change in Paraffin–Oxygen Hybrid Rocket Engines	JOURNAL OF PROPULSION AND POWER	2023
Simplified Numerical Modeling of Film Cooling and Mixture Ratio Bias in Liquid Rocket Thrust Chambers	Proceedings of the Aerospace Europe Conference 2023 - 10th EUCASS - 9th CEAS	2023
Experimental and Numerical Analysis of Transient Erosion in Hybrid Rockets	Proceedings of the International Symposium on Space Technology and Science (ISTS)	2023

ERC

PE8_1

Interessi di ricerca

Hybrid Rocket Engines, Computational Fluid Dynamics, Liquid Rocket Engines, Hypersonic Reentry